U.S. patent number 5,805,975 [Application Number 08/838,677] was granted by the patent office on 1998-09-08 for satellite broadcast receiving and distribution system.
Invention is credited to Austin S. Coker, Jr., James A. Green, Sr..
United States Patent |
5,805,975 |
Green, Sr. , et al. |
September 8, 1998 |
Satellite broadcast receiving and distribution system
Abstract
The present invention provides a satellite broadcast receiving
and distribution system that will permit for the transmission of
vertical and horizontal or left-hand circular and right-hand
circular polarization signals simultaneously via a single coaxial
cable. The system of the present invention will accommodate two
different polarity commands from two or more different sources at
the same time. This satellite broadcast receiving and distribution
system of the present invention will provide for the signals
received from the satellite to be converted to standard frequencies
so as to permit for signals to travel via existing wiring which the
present day amplifiers can transport in buildings, high-rises,
hospitals, and the like so that satellite broadcasting can be
viewed by numerous individuals by way of a single satellite
antenna.
Inventors: |
Green, Sr.; James A.
(Tallahassee, FL), Coker, Jr.; Austin S. (Tallahassee,
FL) |
Family
ID: |
23558106 |
Appl.
No.: |
08/838,677 |
Filed: |
April 9, 1997 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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394234 |
Feb 22, 1995 |
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Current U.S.
Class: |
455/3.02;
348/E7.05; 348/E7.093; 455/12.1; 725/93; 725/94; 725/97 |
Current CPC
Class: |
H04H
40/90 (20130101); H04N 7/20 (20130101); H04N
7/106 (20130101) |
Current International
Class: |
H04H
1/00 (20060101); H04N 7/10 (20060101); H04N
7/20 (20060101); H04H 001/00 (); H04B
007/185 () |
Field of
Search: |
;455/3.2,4.1,427,428,12.1,14,20,22,179.1 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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4126774 |
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Feb 1993 |
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DE |
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2-140022 |
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May 1990 |
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JP |
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Primary Examiner: Vo; Nguyen
Attorney, Agent or Firm: Carnes, Cona and Dixon
Parent Case Text
This is a Continuation-In-Part of application Ser. No. 08/394,234,
filed Feb. 22, 1995, now abandoned.
Claims
We claim:
1. A satellite broadcasting system comprising:
a satellite dish coupled to a low-noise block converter;
said low-noise block converter is coupled to a first means of
converting vertical polarization signals and horizontal
polarization signals or left-hand circular polarization signals and
right-hand circular polarization signals from a satellite and
transmitting simultaneously via a single coaxial cable for enabling
two different frequencies and polarities to be transmitted
simultaneously via said single coaxial cable;
a second means is coupled to said first means;
said second means converts said vertical polarization signals and
said horizontal polarization signals or said left-hand circular
polarization signals and said right-hand circular polarization
signals from said first means to its original received frequency
and polarity from said satellite dish;
a satellite receiver is coupled to said second means; and
a source is coupled to said satellite receiver.
2. A satellite system as in claim 1 wherein a power source is could
to said first means and said power source powers said first
means.
3. A satellite system as in claim 1 wherein said second means
provides for said signals to be converted separately and
independently to said satellite receiver by a transmitting
means.
4. A satellite system as in claim 1 wherein said second means
provides for a transmitting means for said signals to be
selectively converted to said satellite receiver via a first cable
coupled to said second means.
5. A satellite system as in claim 4 wherein said transmitting means
further includes a polarity switch for permitting said signals to
be selectively converted to said satellite receiver.
6. A satellite system as in claim 1 wherein said first means
includes a first converting system for converting said signals of a
first direction to a desired first frequency and polarization and a
second converting system for converting said signals of a second
direction to a desired second frequency and polarization.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates generally to a satellite broadcasting
receiving and distribution system and more particularly to a
broadcasting receiving and distribution system that will allow for
the transmission of vertical and horizontal or left-hand circular
and right-hand circular polarization signals to be transmitted
simultaneously via a single coaxial cable.
2. Description of the Prior Art
Satellite broadcasting has become very popular throughout the
United States. Conventionally, broadcast signals are transmitted
through an artificial satellite at very high frequencies. These
frequencies are generally amplified and are processed by a
particular device after received by an antenna or antennas and
prior to application to a conventional home television set or the
like.
Typically, broadcasting systems comprises an outdoor unit,
generally associated with the antenna, and an indoor unit,
generally associated with the television set, or the like. Both
units, indoor and outdoor, are coupled via a coaxial cable.
A problem associated with these types of systems is that they are
designed to accept signals through a line of sight. Accordingly, if
the satellite is not visual from a building, then the signal cannot
be transmitted. Thus, these systems are rendered useless for
high-rises, hospitals, schools, and the like. These systems are
limited in usage, and, as such, can only be utilized in residential
homes.
As an example, U.S. Pat. No. 5,301,352, issued to Nakagawa et al.
discloses a satellite broadcast receiving system. The system of
Nakagawa et al. includes a plurality of antennas which,
respectively, include a plurality of output terminals. A
change-over divider is connected to the plurality of antennas and
includes a plurality of output terminals. A plurality of receivers
are attached to the change-over divider for selecting one of the
antennas. Though this system does achieve one of its objects by
providing for a simplified satellite system, it does, however,
suffer a major short-coming by not providing a means of receiving
satellite broadcasting for individuals who are not in the direct
line of sight to the antennas. This system is silent to the means
of simultaneously transmitting vertical and horizontal polarized
signals via a single coaxial cable.
U.S. Pat. No. 5,206,954, issued to Inoue et al. and U.S. Pat. No.
4,509,198 issued to Nagatomi both disclose yet another satellite
system that includes an outdoor unit that is connected to a channel
selector. In this embodiment, the satellite signal receiving
apparatus receives vertically and horizontally polarized radiation
signals at the side of a receiving antenna. The signals are then
transmitted, selectively, to provide for either one of the
vertically or horizontally polarized signals to be transferred.
Hence, utilizing a switch allow for only one polarity to be
transmitted. This design and configuration provides for one coaxial
cable to be utilized, but does not provide for the vertical and
horizontal signals to be transmitted simultaneously. This system
selectively transmits the desired signals and polarities.
Systems have been attempted for transferring two frequencies on the
same co-axial cable. Frequencies of the same polarity can easily be
transmitted via a single co-axial cable, however, transmitting two
signals, from two sources, each of different polarities can be a
challenge. In some satellite configuration systems, once a timing
diagram is plotted. For the signals to be transmitted, it is seen
that a forbidden path occurs between frequencies of 950 MHz and
1070 MHz. Inherently prohibiting the frequencies within that range
to be transmitted successfully. Hence, it is desirable to obtain a
system which will not allow for conversion to occur at frequencies
of the forbidden conversion.
As seen in German Patent Number DE4126774-A1, signals can be fail
within the range of the forbidden path, thereby, providing for a
non-working system. Additionally, this product, like the assembly
disclosed in Japanese Application No. 63-293399 both disclose a
system which receives a single signal and demultiplexed them into
vertical and horizontal polarized signals. These systems, are
complex and require a numerous amount of components in order to
employ the invention. This increase in components will inherently
cause an increase in component failure. Further, these systems fail
to disclose a means of reconverting the signals into their original
frequency and polarity, a necessity for satellite systems.
Consequently, the system provides a signal which will not maintain
its respective polarity.
Accordingly, it is seen that none of these previous efforts provide
the benefits intended with the present invention, such as providing
a broadcasting receiving and distribution system that will allow
for the transmission of vertical and horizontal or left-hand
circular and right-hand circular polarization signals to be
transmitted successfully and simultaneously via a single coaxial
cable. Additionally, prior techniques do not suggest the present
inventive combination of component elements as disclosed and
claimed herein. The present invention achieves its intended
purposes, objectives and advantages over the prior art device
through a new, useful and unobvious combination of component
elements, which is simple to use, with the utilization of a minimum
number of functioning parts, at a reasonable cost to manufacture,
assemble, test and by employing only readily available
material.
SUMMARY OF THE INVENTION
The present invention provides a satellite broadcast receiving and
distribution system that will permit for the transmission of
vertical and horizontal or left-hand circular and right-hand
circular polarization signals simultaneously via a single coaxial
cable. The system of the present invention will accommodate two
different polarity commands from two or more different sources at
the same time. This satellite broadcast receiving and distribution
system of the present invention will provide for the signals
received from the satellite to be converted to standard frequencies
so as to permit for signals to travel via existing wiring which the
present day amplifiers can transport in buildings, high-rises,
hospitals, and the like, so that satellite broadcasting can be
viewed by numerous individuals by way of a single satellite
antenna.
The satellite broadcast system of the present invention comprises a
satellite antenna which receives the polarized signals, a head-in
frequency processor for converting the polarized signals, a single
co-axial cable for transmitting the converted signal, a head-out
receiver processor for re-converting the signals to their original
frequency and polarity, and a source, which receives the signals in
their respective original frequency and polarity. Structurally, the
head-in frequency processor is coupled to the head-out receiver
processor via the single co-axial cable. The source is coupled to
the head-out receiver processor.
Hence, to allow for successful conversion, the head-in processor
converts the received signals of two different polarities to
frequencies which permit for transmission simultaneously. The
head-in processor will also accommodate two different polarity
commands from two or more different sources at the same time via
the single cable.
The single cable couples the head-in processor to the head-out
processor. Once in the head-out processor, the signals are
re-converted to their original state for transmission to the source
(i.e. television).
Accordingly, it is the object of the present invention to provide
for a satellite broadcast receiving and distribution system which
will overcome the deficiencies, shortcomings, and drawbacks of
prior satellite broadcast systems and signals and polarity transfer
methods.
It is another object of the present invention to provide for a
satellite broadcast receiving and distribution system that will
convert different frequencies and different polarized signals in
order to permit the signals to be transmitted via a single coaxial
cable.
Another object of the present invention is to provide for a
satellite broadcast receiving and distribution system that will
provide service to mid/high-rise office buildings, condominiums,
schools, hospitals and the like via a single satellite.
Still another object of the present invention, to be specifically
enumerated herein, is to provide a satellite broadcast receiving
and distribution system in accordance with the preceding objects
and which will conform to conventional forms of manufacture, be of
simple construction and easy to use so as to provide a system that
would be economically feasible, long lasting and relatively trouble
free in operation.
Although there have been many inventions related to satellite
broadcast receiving and distribution systems, none of the
inventions have become sufficiently compact, low cost, and reliable
enough to become commonly used. The present invention meets the
requirements of the simplified design, compact size, low initial
cost, low operating cost, ease of installation and maintainability,
and minimal amount of training to successfully employ the
invention.
The foregoing has outlined some of the more pertinent objects of
the invention. These objects should be construed to be merely
illustrative of some of the more prominent features and application
of the intended invention. Many other beneficial results can be
obtained by applying the disclosed invention in a different manner
or modifying the invention within the scope of the disclosure.
Accordingly, a fuller understanding of the invention may be had by
referring to the detailed description of the preferred embodiments
in addition to the scope of the invention defined by the claims
taken in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a block diagram illustrating the components used for the
satellite broadcast receiving and distribution system according to
the present invention.
FIG. 2 is a block diagram representing a first embodiment of the
head-in frequency processor and two embodiments of the head-out
frequency processor used for the satellite broadcast receiving and
distribution system according to the present invention.
FIG. 3a is a schematic diagram of the down converter used for the
satellite broadcast signal receiving and distribution system
according to the present invention.
FIG. 3b is a schematic diagram of the up converter used for the
satellite broadcast signal receiving and distribution system
according to the present invention.
FIG. 4 is a block diagram of the second embodiment of the satellite
broadcast signal receiving and distribution system according to the
present invention.
FIG. 5 is a block diagram of the third embodiment of the satellite
broadcast signal receiving and distribution system according to the
present invention.
Similar reference numerals refer to similar parts throughout the
several views of the drawings.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As illustrated in FIG. 1, the satellite system 10 of the present
invention includes a receiving satellite 12 that will transmit
signals (Vertical-polarized signals and Horizontal-polarized
signals or left-hand circular and right-hand circular polarization
signals) to a head-in equipment frequency processor 14. It is at
this head-in equipment frequency processor 14 where the signals are
received simultaneously and then transmitted via a single coaxial
cable 16 to the head-out receiver processor 18. This will enable
for the single coaxial cable 16 to transmit signals of two
different polarities and frequencies simultaneously. From the
head-out frequency processor the signals are reconverted to its
original state and then transmitted to a source 20. As seen in FIG.
1, the two different polarities (Vertical-polarized signals and
Horizontal-polarized signals or left-hand circular and right-hand
circular polarization signals) are transported to the source via
separate cables 22a and 22b, respectively.
The system of the present invention includes separate embodiments,
and the first embodiment is illustrated in FIG. 2. As seen in the
first embodiment of the present invention 10a, there is shown a
head-in frequency processor 14a couple to either a first head-out
frequency processor 18a or a second head-out frequency processor
18b.
It is noted that FIG. 2 illustrates the head-in processor 14a to be
coupled to two separate head-out processors 18a and 18b,
respectively. This is shown for illustrative purposes only. In
actuality, only one head-out receiver processor is utilized with
the head-in processor 14a. The type and embodiment used for the
head-out receiver processor is dependent to the combination of the
satellite receiver and source that is utilized.
As seen in FIG. 2, the head-in equipment frequency processor 14a
will receive two signals or two separate polarities and convert
them to separate frequencies for enabling transmission via a single
coaxial cable 16a.
A low-noise block converter (LNB) 24 will receive the signals from
the satellite 12. This LNB 24 is conventional and is used for
amplifying the respective polarized signals (Vertical-polarized
signals and Horizontal-polarized signals or left-hand circular and
right-hand circular polarization signals). Accordingly, after
signals are received, they pass the low-noise block converter 24,
to provide for the signals to enter the head-in equipment frequency
processor 14a (illustrated in FIG. 2 as dashed lines) via conduits
26a and 26b, respectively.
The head-in equipment frequency processor 14a, illustrated in FIG.
2, provides for the signals to be converted, via converters 28 and
30, to the frequencies which the present day amplifiers can
transport. In this stage of the system, the object is to convert
the signals of one polarity up (via converter 30) and to convert
the signals of second polarity down (via converter 28). This will
render the converted signals to be transmitted without emerging
into the forbidden frequency conversion.
From the conduits 26a and 26b, the signals are transmitted to a
first converter or down converter 28 and a second converter or up
converter 30. These frequency converters, 28 and 30, respectively,
convert the entered frequencies to a frequency which present day
amplifies can transport. The converters will be discussed in
further detail in FIGS. 3a and 3b. The utilization of two
converters permit for the acceptance of two signals or polarized
transponders that are of a different frequency.
In the down converting means 28, the transponder is converted down
to a specified frequency. The specified frequency is the frequency
that is required for the present day amplifiers for transportation.
The newly converted frequencies are amplified through the
amplifying means 32a. At means 32a, the converted frequencies are
amplified so not to create second harmonics. These signals are then
transferred to a conventional four way splitter 34a.
In the up converting means 30, the transponders are converted up to
a specified frequency. The converted frequencies then are converted
down via a down converter 36. This process of converting up and
then down provides for frequencies to be converted without
difficulties and avoiding the forbidden conversion area.
The convert ed signals are transferred to the four way splitter 34a
in ordered to combine the frequency of the amplified signal of 32a
and frequency from converter 36. To synchronized the system, the
frequencies from the phase lock loop (PLL) transmitter 38a are
transmitted to the splitter 34a.
From the splitter 34a, the signals are passed through an AC power
separator 40 which routes 60 Volts power to a DC power supply of 18
Volts. This will permit for the dual frequencies from the satellite
dish 12 to be transmitted simultaneously via a single coaxial cable
16a. Dependent upon the length of the cable, an optional
conventional amplifier 42 can be coupled thereto. Power from a
power source 44 is inserted into the lines via a power inserter 46.
The signals are amplified, as needed, with additional amplifiers
48. It is noted that the amplifiers are optional and are dependent
to the distance that the head-in frequency processor 14a is located
from the head-out frequency processor 18a or 18b. The power supply
and power source 11 en energizes the head-in frequency processor
14a.
From the single coaxial cable 16a, the signals are adjusted via a
tap 50a to permit for the appropriate decibels that are required
for the head-out processor 18a or 18b.
The head-out frequency processor used for the head-in processor 14a
illustrated in FIG. 1, can include two embodiments, dependent upon
the embodiment for the source in combination with the satellite
receiver.
The first embodiment for the head-out frequency processor is
illustrated in FIG. 2 by way of dash line 18a. As seen in this
embodiment, the simultaneously transmitted signals enter the
processor via conduit 16b. The conduit 16b is coupled to a
conventional four (4) way splitter 34b. A conventional phase lock
loop (PLL) receiver 56a is coupled to the splitter 34b to permit
for the signals to be locked to the proper and desired frequencies.
From the splitter 34b the first frequency is transmitted to a first
converter 58a in order to permit for the signals or transponders to
be converted up to a specified frequency. This up converted signal
from the first converter or up converter 58a is then transmitted to
the satellite receiver by way of a conduit 22b.
The second frequencies are transmitted to a first or up converter
52a and then are transported to a second or down converter 54a.
This will permit for the signals to be converted to the desired
frequency. This second or down converter is coupled to the
satellite receiver 21 via conduit 22a. The signals from down
converter 54a and from up converter 58a are in the original state,
both frequency and polarity, when transmitted from the satellite to
the head-in processor 14a, via lines 26a and 26b. The re-converted
signals, frequencies and polarity in its original state, are
transmitted to the satellite receiver 21 via lines 22a and 22b. The
satellite receiver 21 is coupled to a source 20 (illustrated as a
television) to provide for proper transmission of the signals. The
transmission line between the satellite receiver 21 and source 20
is illustrated but not labeled.
Hence, it is seen that the head-in processor converted the signals
to different frequencies to enable the transmission of two separate
polarized signals via a single co-axial cable to a head-out
processor. From the head-out processor, the signals are
re-converted to their original state, which was received via lines
26a and 26b. For example, with satellite systems, frequencies
typically range between 950-1450 MHz. If the satellite transmits a
frequency of 1450 for both the horizontal and vertical polarities,
then one of the polarities, such as horizontal, is converted down
to 560 MHz via converter 28. The second frequency of the second
polarity, such as vertical, is first converted up to 2010 and then
back down to 1070, via converters 30 and 36, respectively. Such a
conversion allows for the two frequencies of two different
polarities, 560 MHz (horizontal) and 1070 MHz (vertical), to be
transmitted simultaneously on a single co-axial cable (16a and
16b).
As illustrated, this head-out frequency processor is the reverse
process of the head-in processor. This is to provide for the
signals to reconverted to its original frequencies so as to provide
for the satellite receiver 21 and source 20 to accept the signals.
The single cable 16b accepts the signals at frequencies different
than that of the source. Accordingly, the head-out processor must
re-convert the signals to the frequencies that are utilized by the
source 20.
An alteration of the satellite receiver requires an alteration in
the head-out receiver processor. This alteration is illustrated in
FIG. 2 and is shown in outline designated as reference 18b. In this
design and configuration, the satellite receiver utilizes only one
wire and accepts only one type of signal, selectively, such as only
left-hand circular or only right hand circular polarized
signals.
As seen, the frequencies are tapped via 50b. The tap 50b is coupled
to the head-out processor 18b via line 16b which is connected to a
four (4) way splitter 34c. To provide for the signals to be locked
in proper frequencies, the four way splitter is coupled to a phase
lock loop (PLL) receiver 56b.
From the splitter 34c, the first signal of a first polarity is
transmitted to a first or up converted 52b and then is transmitted
to a second or down converter 54b. The conversion of the signals
from up to down provides the benefit of converting the frequency
without any mishap or error. This method of conversion will avoid
the forbidden conversion area as well as provide for the original
received frequency and polarity of the signals.
The signals of the second frequency and second polarity are
transmitted to an up converter 58b which will inherently convert
the signals to its original received frequency while maintaining
its polarity. A polarity switch 60 is connected to converters 52b,
54b, and 58b for coupling the head-out processor to the satellite
receiver via a single cable 22c and a joining means, which is a
four way splitter 34d. The satellite receiver 21 is connected by
way of a line (illustrated, but not labeled) to a source 20. In
this embodiment, the switch 60 is used to determine which polarity
will enter into the head-out processor 18b.
In the embodiments shown above, the satellite receiver 21 and
source 20 are conventional components and as such, their schematics
are not shown in further detail. The up and down converters used in
the embodiment above will be discussed in further detail in FIG. 3a
and FIG. 3b. FIG. 3a represents the schematic rendering of the down
converters (28, 36, 54a, and 54b) and FIG. 3b represents the
schematic rendering of the up converters (30, 52a, 52b, 58a, and
56b).
As seen in the schematic diagram of FIG. 3a, the signal enters the
down converter via line L1. The entered signal passes through a
first capacitor C1 which is coupled to an amplifier AMP. After
passing the amplifier AMP, the signal passes a second capacitor C2
before entering a first low pass filter LPF1. This first LPF1 is
coupled to a mixer which is coupled to a second LPF2. This second
LPF2 is connected to a third capacitor C3 which is coupled to a
second choke CH2. The mixer is also connected to an oscillator OSC.
The oscillator is coupled to a PPL. The first capacitor C1 is also
connect to a first choke CH1. Capacitors C, C1, C2, C3 are coupled
to the amplifier, oscillator, phase lock lope PPL, and the second
low pass filter. Resistors R are coupled to the amplifier,
oscillator, first low pass filter and mixer. Chokes are also
coupled in series with capacitors to provide for the chokes to be
parallel with the amplifier AMP and the second low pass filter,
respectively. As seen the chokes CH1 and CH2 (inductors) and
capacitors C are a DC bypass filter network and provide a DC path
and enables passing DC power to the antenna electronics.
The up converter is disclosed in FIG. 3b. As seen in this drawings,
the signal enters the up converter via a first line L2. The
converter further includes an amplifier AMP that is coupled to a
first low pass filter LP1. The amplifier is also coupled to an
oscillator OSC. The oscillator and the first low pass filter are
connect to a mixer. This mixer is coupled to a high pass filter
HPF. The oscillator is also connected with a phase lock loop
receiver PLL. A second amplifier AMP2 is coupled to the high pass
filter HPF. A second low pass filter LPF2 is coupled to the second
amplifier. Capacitors are coupled to the first amplifier, first
lower pass filter, and a the amplifier. Resistors R are coupled
other first and second amplifiers, oscillator, first low pass
filter, and mixer. Chokes are also used in this circuit. The first
choke is coupled to a capacitor which is coupled to the first
amplifier. The second chock is coupled to the phase lock loop.
Simplifying the head out processor described above, will provide
another embodiment for the satellite broadcast receiving and
distribution system. This system is illustrated in further detail
in FIG. 4. This embodiment simplifies the above describe
embodiments and also provides a device which avoids the forbidden
path. Alteration for this embodiment occurs in the head-in
equipment frequency processor 14b and the head-out frequency
processor 18c.
As with the first embodiment, a low-noise block converter (LNB) 24
will receive the signals from the satellite 12. This LNB 24, as
stated previously, is conventional and is used for amplifying the
respective polarized signals (Vertical-polarized signals and
Horizontal-polarized signals or left-hand circular and right-hand
circular polarization signals). Hence, after signals are received,
they pass the low-noise block converter 24, to provide for the
signals to enter the head-in equipment frequency processor 14b
(illustrated in FIG. 4 as dashed lines) via conduits 26a and 26b,
respectively.
The head-in equipment frequency processor 14b, provides for the
signals to be converted, via converters 28 and 30, as identified
for the first embodiment. Thereby providing a system which includes
frequencies that the present day amplifiers can transport. In this
stage of the system, the object is to convert the signals of one
polarity up (via converter 30) and to convert the signals of second
polarization down (via converter 28).
From the conduits 26a and 26b, the signals are transmitted to a
first converter or down converter 28 and a second converter or up
converter 30. These frequency converters, 28 and 30, respectively,
convert the entered frequencies to a frequency which present day
amplifies can transport. The converters have been discussed in
further detail in FIGS. 3a and 3b. The utilization of two
converters permit for the acceptance of two signals or polarized
transponders that are of a different frequency.
In the down converting means 28, the transponder is converted down
to a specified frequency. The specified frequency is the frequency
that is required for the present day amplifiers for transportation.
Though not illustrated, the newly converted frequencies are
amplified through the amplifying means, as illustrated in FIG. 2
via element 32a. At the amplifying means 32, the converted
frequencies are amplified so not to create second harmonics. These
signals are then transferred to a conventional two-way splitter
34c.
In the up converting means 30, the transponders are converted up to
a specified frequency. The converted signals are transferred to the
two way splitter 34c in order to combine the frequency of the
amplified signals. To synchronized the system, the frequencies from
the phase lock loop (PLL) transmitter 38a are transmitted to the
splitter 34c.
From the splitter 34c, the signals are passed through a
conventional tilt and gain 62. This will permit for the dual
frequencies from the satellite dish 12 to be transmitted
simultaneously via a single coaxial cable 16a. Dependent upon the
length of the cable, an optional conventional amplifier 42 can be
coupled thereto. Power from a power source 44 is inserted into the
lines via a power inserter 46. The signals are amplified, as
needed, with additional amplifiers 48. It is noted that the
amplifiers are optional and are dependent to the distance that the
head-in frequency processor 14b is located from the head-out
frequency processor 18c. The power supply and power source 11
energize the head-in frequency processor 14b.
From the single coaxial cable 16a, the signals are adjusted via a
tap 50a to permit for the appropriate decibels that are required
for the head-out processor 18c.
The head-out frequency processor used for the head-in processor 14b
is illustrated in by way of dash line 18c. As seen in this
embodiment, the simultaneously transmitted signals enter the
processor via conduit 16b. The conduit 16b is coupled to a
conventional two (2) way splitter 34d. A conventional phase lock
loop (PLL) receiver 56a is coupled to the splitter 34d to permit
for the signals to be locked to the proper and desired frequencies.
From the splitter 34d the first frequency is transmitted to a first
converter 52c in order to permit for the signals or transponders to
be converted up to a specified frequency. The converted signals
from the first converter or up converter 52c are then transmitted
to the satellite receiver by way of a conduit 22a.
The second frequencies are transmitted to a down converter 54c.
This will permit for the signals to be converted to the desired
frequency. This second or down converter is coupled to the
satellite receiver 21 via conduit 22b. The signals from down
converter 54c and from up converter 52c are in the original state,
both frequency and polarity, when transmitted from the satellite to
the head-in processor 14b, via lines 26a and 26b. The re-converted
signals, frequencies and polarity in its original state, are
transmitted to the satellite receiver 21 via lines 22a and 22b. The
satellite receiver 21 is coupled to a source 20 (illustrated as a
television) to provide for proper transmission of the signals. The
transmission line between the satellite receiver 21 and source 20
is illustrated but not labeled.
Hence, it is seen that the head-in processor converted the signals
to different frequencies to enable the transmission of two separate
polarized signals via a single co-axial cable to a head-out
processor. From the head-out processor, the signals are
re-converted to their original state, which was received via lines
26a and 26b. The above identified embodiment is ideal for long
distant use, i.e. exceeding 1000 feet. However, for shorter
distance, i.e. less than 1000 feet, the components can be
simplified again to provide for a device which is ideal for use in
apartments or the like.
As seen in FIG. 5, the present invention includes the head-in
equipment frequency processor 14c and the head-out frequency
processor 18d.
As with the first the previous embodiments, a low-noise block
converter (LNB) 24 will receive the signals from the satellite 12.
This LNB 24, as stated previously, is conventional and is used for
amplifying the respective polarized signals (Vertical-polarized
signals and Horizontal-polarized signals or left-hand circular and
right-hand circular polarization signals). Hence, after signals are
received, they pass the low-noise block converter 24, to provide
for the signals to enter the head-in equipment frequency processor
14c (illustrated in FIG. 5 as dashed lines) via conduits 26a and
26b, respectively.
As seen, this head-in equipment frequency processor 14c is
simplified. The head-in equipment frequency processor 14c, provides
for signals of one frequency to be converted, up via converter 30,
as identified for the first embodiment. Thereby providing a system
which includes frequencies that the present day amplifiers can
transport. In this stage of the system, the object is to convert
the signals of one polarity up (via converter 30). The signal of
the second polarity is amplified via conventional amplifier
32a.
From the conduits 26a and 26b, the signals are transmitted to a
first converter or up converter 30 and a amplifier 32a. The down
converters have been discussed in further detail in FIG. 3a.
From the amplifier and up converter, the signals are transferred to
a conventional hybrid mixer 36a. From the mixer, the signals pass a
diplexer 64. Signifies exit the diplexer via a single co-axial
cable 16a.
From the single coaxial cable 16a, the signals can be adjusted via
a tap (illustrated, but not labeled) to permit for the appropriate
decibels that are required for the head-out processor 18d.
The head-out frequency processor used for the head-in processor 14c
is illustrated in by way of dash line 18d. As seen in this
embodiment, the simultaneously transmitted signals enter the
processor via conduit 16b. The conduit 16b is coupled to a
conventional mixer 36b. From the mixer 36b the first frequency is
transmitted to an amplifier 32b and the second frequency of a
different polarity is transferred to a down converter 52d for
converting the frequency to its original state.
The re-converted signals, frequencies and polarity in its original
state, is transmitted to the satellite receiver 21 via lines 22a
and 22b. The satellite receiver 21 is coupled to a source 20
(illustrated as a television) to provide for proper transmission of
the signals. The transmission line between the satellite receiver
21 and source 20 is illustrated but not labeled.
Hence, it is seen that the head-in processor converted the signals
to different frequency to enable the transmission of two separate
polarized signals via a single co-axial cable to a head-out
processor. From the head-out processor, the signals are
re-converted to their original state, which was received via lines
26a and 26b. The above
The satellite system of the present invention will permit for two
signals of different frequency and polarities to travel
simultaneously via a single coaxial cable. The use of this will
provide for a satellite system that is versatile, economical and
compact. The usage of the single cable permits for a system that
can accept satellite broadcasting in places that were previously
render impossible. These places include mid/high-rise office
buildings, condominiums, hospitals, schools, etc. The unique design
and configuration enables the signals to be transmitted via the
existing wiring of the buildings. The only renovations that may
need to be done is the upgrading of the existing amplifiers.
While the invention has been particularly shown and described with
reference to an embodiment thereof, it will be understood by those
skilled in the art that various changes in form and detail may be
made without departing from the spirit and scope of the
invention.
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